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NASA Technical Reports Server (NTRS) 19930018062: Design verification test matrix development for the STME thrust chamber assembly

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NASA Technical Reports Server (NTRS) 19930018062: Design verification test matrix development for the STME thrust chamber assembly

by
NASA Technical Reports Server (NTRS)

Publication date
Topics
NASA Technical Reports Server (NTRS), ADVANCED LAUNCH SYSTEM (STS), DESIGN ANALYSIS, PROVING, ROCKET ENGINE DESIGN, SPACE SHUTTLE MAIN ENGINE, THRUST CHAMBERS, COMBUSTION CHAMBERS, INJECTORS, ROCKET NOZZLES, Dexter, Carol E., Elam, Sandra K., Sparks, David L.,
Collection
NASA_NTRS_Archive; additional_collections
Language
English
This report presents the results of the test matrix development for design verification at the component level for the National Launch System (NLS) space transportation main engine (STME) thrust chamber assembly (TCA) components including the following: injector, combustion chamber, and nozzle. A systematic approach was used in the development of the minimum recommended TCA matrix resulting in a minimum number of hardware units and a minimum number of hot fire tests.
Addeddate
2016-10-03 22:30:24
Identifier
NASA_NTRS_Archive_19930018062
Identifier-ark
ark:/13960/t4wh7gx8j
Ocr
ABBYY FineReader 11.0
Pages
42
Ppi
600
Year
1993

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